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Preliminary design of a small-sized flapping UAV: II. Kinematic and structural aspects

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Abstract

The design of the actuating mechanism of a biologically inspired flapping wing UAV is addressed. Several configurations able to reproduce the desired flapping-wing kinematics are analyzed and an optimization study is conducted to select the best configuration. The optimization results are used as the starting point for the design of the different structural components of the flapping mechanism. During the mechanism design stage, the linkages are optimized to match the desired wing’s motion during a flapping cycle. A structural and durability analysis is then conducted to verify that the mechanism and its components are able to withstand the aerodynamic and inertial loads.

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References

  1. Madangopal R, Khan ZA, Agrawal SK (2005) Biologically inspired design of small flapping wing air vehicles using four-bar mechanisms and quasi-steady aerodynamics. J Mech Des 127:809–816

  2. Malik AM, Khalid MSU, Barlas F (2010) Modeling and simulation of kinematics for an active flapping and pitching mechanism. In: Proceedings of the World Congress on Engineering 2010 vol II WCE 2010, June 30–July 2, 2010, London, UK

  3. Zbikowski R, Galinski C, Pedersen CB (2005) Four-bar linkage mechanism for insectlike flapping wings in hover: concept and an outline of its realization. J Mech Des 127(4):817–824

    Article  Google Scholar 

  4. Kempf A (1999) Patent nFR2776937, France

  5. Larijani RF, DeLaurier JD (2001) nonlinear aeroelastic model for the study of flapping wing flight, fixed and flapping wing aerodynamics for micro air vehicle applications. In: Mueller TJ (ed) Progress in astronautics and aeronautics, vol 195. AIAA, Reston, pp 399–420

    Google Scholar 

  6. DeLaurier JD, Harris JM (1993) A study of mechanical flapping-wing flight. Aeronaut J R Aeronaut Soc 97(968):277–286

  7. DeLaurier JD (1993) An aerodynamic model for flapping-wing flight. Aeronaut J R Aeronaut Soc 97(964):125–130

  8. DeLaurier JD (1999) The development and testing of a full-scale piloted ornithopter. Can Aeronaut Space J 45(2):72–82

  9. http://www.festo.com/cms/en_corp/11369.htm

  10. Send W, Fischer M, Jebens K, Mugrauer R, Nagarathinam A, Scharstein F (2012) Artificial hinged-wing bird with active torsion and partially linear kinematics. Congress ICAS 2012

  11. Guerrero JE, Pacioselli C, Pralits JO, Negrello F, Silvestri P, Lucifredi A, Bottaro A (2014) Preliminary design of a small-size flapping UAV. I. Aerodynamic performance and static longitudinal stability, to be submitted (2014)

  12. DeLaurier J et al Ornithopter project. Available at: http://www.ornithopter.net

  13. Ornithopters Patent Collection. Available at: http://www.rexresearch.com/ornithopter/ornithopter.htm

  14. Kempf A, Truefly. Available at:http://truefly.chez.com

  15. Kakuta K, Buteo F4. Available at: http://homepage2.nifty.com/smark/ButeoF4E.htm

  16. Sclater N, Chironis NP (2001) Mechanisms and mechanical devices sourcebook. McGraw-Hill, New York

    Google Scholar 

  17. Schiehlen W et al (1990) Multibody systems handbook. Springer, Berlin

    Book  MATH  Google Scholar 

  18. LMS Virtual Lab R12 On-Line Help, Leuven, Belgium (2013)

  19. http://www.maxonmotor.it/maxon/view/catalog

  20. Craig R, Bampton M (1968) Coupling of substructures for dynamics analysis. AIAA J 6(7):1313–1319

    Article  ADS  MATH  Google Scholar 

  21. Stephens RI, Fatemi A, Stephens RR, Fuchs HO (2001) Metal fatigue in engineering, 2nd edn. Wiley, New Jersey

    Google Scholar 

  22. LMS Samcef Field 8.4 On-Line Help, Leuven, Belgium (2013)

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Correspondence to A. Bottaro.

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Negrello, F., Silvestri, P., Lucifredi, A. et al. Preliminary design of a small-sized flapping UAV: II. Kinematic and structural aspects. Meccanica 51, 1369–1385 (2016). https://doi.org/10.1007/s11012-015-0309-7

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  • DOI: https://doi.org/10.1007/s11012-015-0309-7

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